AIRCRAFT LANDING GEAR, AIRCRAFT, AND RELATED METHODS

An aircraft landing gear structure (18, 70, 152) according to the present disclosure includes a strut assembly (71, 100, 154) and a wheel assembly (20) operatively coupled to the strut assembly. The strut assembly includes an upper tubular housing (26) and a lower tubular housing (28) configured to...

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Bibliographic Details
Main Authors CUSWORTH, James E, JOHNSON, Richard Kevin, MELLOR, Mitchell Loren Ray, SIMPSON, Mark Nicholas, SONNENBURG, George, COTTET, Justin
Format Patent
LanguageEnglish
French
German
Published 29.08.2018
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:An aircraft landing gear structure (18, 70, 152) according to the present disclosure includes a strut assembly (71, 100, 154) and a wheel assembly (20) operatively coupled to the strut assembly. The strut assembly includes an upper tubular housing (26) and a lower tubular housing (28) configured to be longitudinally translated with respect to the upper tubular housing such that the overall length of the strut assembly is transitioned between an extended configuration (74) and a retracted configuration(76) for stowage during flight. The wheel assembly includes a forward link (36) pivotally coupled to the upper tubular housing (26) and a truck beam (34) that is pivotally coupled to the lower tubular housing (28) such that translation of the lower tubular housing with respect to the upper tubular housing causes pivoting of the forward link and the truck beam with respect to one another, thereby tilting and/or raising a wheel of the wheel assembly (20) with respect to the upper tubular housing.
Bibliography:Application Number: EP20180158455